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SHUTTLE AVIONICS Design Constraints & Considerations A Guide Book Compiled by C.M. McCleskey/NASA Approved by M.A. O’Neal for the Strategic Avionics Technology Working Group (SATWG) April 25, 1995 |
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SHUTTLE AVIONICS Design Constraints & Considerations A Guide Book Compiled by C.M. McCleskey/NASA Approved by M.A. O’Neal for the Strategic Avionics Technology Working Group (SATWG) April 25, 1995 |
Objective - Consolidate within one report the operational Constraints and Considerations for launch site testing of the present Shuttle Avionics systems.
- Constraint - Testing that requires special vehicle configurations and ground support equipment configurations.
- Consideration - Testing configurations that have driven special infrastructure/ resource requirements, or have high failure rates.
Purpose - To provide to the designers of future avionics systems the information required to possibly design out these concerns.
For questions or comments on this guide contact Carey McCleskey, NASA KSC, Shuttle Avionics and Advanced Projects, at carey.mccleskey-1@ksc.nasa.gov or 407-861-3775.
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Edgar Zapata, NASA Kennedy Space Center
Shuttle Process Engineering Directorate, Fluid Systems Division
